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US3942847A - Temperature compensating ceramic metal bearing systems - Google Patents

Temperature compensating ceramic metal bearing systems Download PDF

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Publication number
US3942847A
US3942847A US05/434,645 US43464574A US3942847A US 3942847 A US3942847 A US 3942847A US 43464574 A US43464574 A US 43464574A US 3942847 A US3942847 A US 3942847A
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United States
Prior art keywords
temperature compensating
ceramic member
bearing
bearing assembly
helical
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Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
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US05/434,645
Inventor
Norman Lawrence Parr
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National Research Development Corp UK
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National Research Development Corp UK
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C17/00Sliding-contact bearings for exclusively rotary movement
    • F16C17/12Sliding-contact bearings for exclusively rotary movement characterised by features not related to the direction of the load
    • F16C17/22Sliding-contact bearings for exclusively rotary movement characterised by features not related to the direction of the load with arrangements compensating for thermal expansion

Definitions

  • This invention relates to temperature compensating bearing assemblies and in particular to temperature compensating ceramic/metal bearing assemblies.
  • the present invention relates to a temperature compensating bearing for a shaft or a like movable member in which an expandible helical ceramic member is employed intermediate between the shaft and a housing therefor.
  • the invention When the invention is applied to a dry bearing assembly required to operate over a wide temperature range it may include a graphitic material located within the space provided by the gap in the expandible helical ceramic member, which graphitic material will then be dispursed over the bearing surfaces during operation if the bearing as a lubricating film of graphite.
  • the expandible helical ceramic member is preferably of silicon nitride and may be fabricated by any of the known fabrication techniques.
  • FIG. 1 is a perspective view of the ceramic helical member
  • FIG. 2 illustrates a bearing in accordance with the present invention
  • FIG. 3 is a perspective view of a modified shaft.
  • an expandible helical ceramic member 1 is designed to operate by expanding and contracting sympathetically with change in shaft diameter with change in temperature whilst maintaining gas clearances with the bearing surfaces on the metal housing 2.
  • the helical gap 3 formed in the helical ceramic member 1 acts also to assist to even out the gas pressure in the bearing and also provide a degree of pumping action.
  • This pumping action can be further enhanced by forming a counter helical groove 4 in the shaft 5, as shown in FIG. 3. It is necessary to provide end sealing arrangements to the bearing, in order to maintain gas pressures within the bearing demanded by the required bearing stiffness, and cover plates 6 fitting close to the surface of the shaft to restrict gas flow are provided for that purpose.
  • separate split collars with close tolerances can be provided at each end of the bearing, as described in U.S. Pat. No. 1,310,274.
  • the helical ceramic member may be formed of silicon nitride by the flame-spray deposition of fine silicon powder onto a polished mandrel previously coated with a soluble release agent, as described in U.S. Pat. No. 1,138,284.
  • the helix is then ground externally, whilst still on the mandrel, and is then released and reaction bonded to silicon nitride by heating in nitrogen and then lightly finished to final dimensions by polishing.
  • the circumferential shots 7 in the helix may be made by stretching thin foil (eg 0.0001 inch) between sets of removable split pegs fitted into the mandrel before spray deposition.
  • the bearing may be self-pressurised due to the counter helical groove in the shaft, assisted by the helical gap in the ceramic helix, or jacking gas may be supplied to the bearing through a conduit 8 passing through the housing.
  • the invention may be used in a modified form for use in rotational or reciprocating shaft dry journal bearings to operate over wide temperature ranges, particularly if a graphic spiral for dispensing graphite films over the surface of the shaft is enclosed in the space provided by the gap in the ceramic helix.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Sliding-Contact Bearings (AREA)
  • Ceramic Products (AREA)
  • Support Of The Bearing (AREA)

Abstract

The invention concerns a temperature compensating bearing for a shaft in which an expandable helical ceramic member is provided between the shaft and the bearing housing. The expandable helical ceramic member functions by expanding and contracting sympathetically with any changes in shaft diameter due to change of temperature of the bearing.

Description

This invention relates to temperature compensating bearing assemblies and in particular to temperature compensating ceramic/metal bearing assemblies.
An alleviation of strict design and operating criteria for bearing technology by the use of inorganic non-metallic to metallic mating surfaces in critical components of bearing systems has been described in British Pat. No. 1,310,274. The precise choice of metallic and inorganic non-metallic components depends upon operating loads, speeds and invironments, but where high temperatures are involved the preferred inorganic non-metallic material must have a combination of high temperature strength, low co-efficient of friction and high resistance to fracture by thermal stress or thermal shock. Such properties are obtainable in reaction-bonded or hotpressed silicon nitride and its derivatives.
One of the chief virtues of using such combinations of materials in gas bearing technology is to permit fortuitous touch-down without causing catastrophic failure by seizing or galling as is normal to total metallic systems. The use of inorganic non-metallic materials with metals will thus permit the possibility of a bearing operation passing from a plain journal unlubricated system to a self-pressurised gas bearing system as shaft speed is increased with or without the use of jacking gas.
The chief problems attendant with the use of mixed metallic/inorganic non-metallic materials in systems expected to operate over temperature ranges is the inherent difference in co-efficients of thermal expansion. In order, therefore, to avoid loss of close tolerance of clearances, or to avoid fracture loads imposed by thermal expansion mismatch, it is necessary to provide means for the sympathetic compensation of dimension changes consequent upon temperature gradients and levels.
The present invention relates to a temperature compensating bearing for a shaft or a like movable member in which an expandible helical ceramic member is employed intermediate between the shaft and a housing therefor.
When the invention is applied to gas bearing assemblies it is very desirable to provide end sealing covers on plates which are arranged to fit closely around the shaft to restrict the loss of gas pressure from within the bearing of gas pressure from within the bearing assembly. Presurisation of the bearing assembly may with advantage be aided by the provision on the bearing surface of the shaft of a helical groove arranged in counterdirection to the helix angle of the expandible helical ceramic member.
When the invention is applied to a dry bearing assembly required to operate over a wide temperature range it may include a graphitic material located within the space provided by the gap in the expandible helical ceramic member, which graphitic material will then be dispursed over the bearing surfaces during operation if the bearing as a lubricating film of graphite.
The expandible helical ceramic member is preferably of silicon nitride and may be fabricated by any of the known fabrication techniques.
In order that the present invention may be more fully understood embodiments thereof will now be described, by way of example, with reference to the accompanying drawings, in which:
FIG. 1 is a perspective view of the ceramic helical member;
FIG. 2 illustrates a bearing in accordance with the present invention; and
FIG. 3 is a perspective view of a modified shaft.
Referring to the drawings, an expandible helical ceramic member 1 is designed to operate by expanding and contracting sympathetically with change in shaft diameter with change in temperature whilst maintaining gas clearances with the bearing surfaces on the metal housing 2. The helical gap 3 formed in the helical ceramic member 1 acts also to assist to even out the gas pressure in the bearing and also provide a degree of pumping action. This pumping action can be further enhanced by forming a counter helical groove 4 in the shaft 5, as shown in FIG. 3. It is necessary to provide end sealing arrangements to the bearing, in order to maintain gas pressures within the bearing demanded by the required bearing stiffness, and cover plates 6 fitting close to the surface of the shaft to restrict gas flow are provided for that purpose. Alternatively, separate split collars with close tolerances can be provided at each end of the bearing, as described in U.S. Pat. No. 1,310,274.
The helical ceramic member may be formed of silicon nitride by the flame-spray deposition of fine silicon powder onto a polished mandrel previously coated with a soluble release agent, as described in U.S. Pat. No. 1,138,284. The helix is then ground externally, whilst still on the mandrel, and is then released and reaction bonded to silicon nitride by heating in nitrogen and then lightly finished to final dimensions by polishing. The circumferential shots 7 in the helix may be made by stretching thin foil (eg 0.0001 inch) between sets of removable split pegs fitted into the mandrel before spray deposition. The bearing may be self-pressurised due to the counter helical groove in the shaft, assisted by the helical gap in the ceramic helix, or jacking gas may be supplied to the bearing through a conduit 8 passing through the housing.
The invention may be used in a modified form for use in rotational or reciprocating shaft dry journal bearings to operate over wide temperature ranges, particularly if a graphic spiral for dispensing graphite films over the surface of the shaft is enclosed in the space provided by the gap in the ceramic helix.
Further specific fabrication techniques for producing silicon nitride bodies that are applicable to the fabrication of the expandible helical ceramic member are described in British Pat. No. 1,021,053 and pending British Pat. No. 52445/72.

Claims (11)

I claim:
1. A temperature compensating bearing assembly for a shaft comprising a bearing housing, and an expandable helical ceramic member located within said bearing housing and providing a bearing surface.
2. A temperature compensating bearing assembly as claimed in claim 1 in which the expandable helical ceramic member is fabricated from silicon nitride.
3. A temperature compensating bearing assembly as claimed in claim 1 in which said bearing surface is comprised in part of the expandable helical ceramic member and in part of a helical spiral of graphitic material, said helical spiral of graphitic material being located in the helical spiral of the expandable helical ceramic member.
4. A temperature compensating bearing assembly as claimed in claim 3 in which the expandable helical ceramic member is fabricated from silicon nitride.
5. A temperature compensating bearing assembly comprising an expandable helical ceramic member located within said bearing housing and providing a first opposed bearing surface and a shaft located within said expandable helical ceramic member and including a second opposed bearing surface opposed to said first bearing surface.
6. A temperature compensating bearing assembly as claimed in claim 5 in which said second opposed bearing surface includes a helical groove arranged in an angled direction in counter-direction to the helix angle of the expandable helical ceramic member.
7. A temperature compensating bearing assembly as claimed in claim 5 including end sealing cover plates located at the ends of the bearing housing and arranged to fit closely around the shaft.
8. A temperature compensating bearing assembly as claimed in claim 6 including end sealing cover plates located at the end of the bearing housing and arranged to fit closely around the shaft.
9. A temperature compensating bearing assembly as claimed in claim 5 in which the expandable helical ceramic member is fabricated from silicon nitride.
10. A temperature compensating bearing assembly as claimed in claim 6 in which the expandable helical ceramic member is fabricated from silicon nitride.
11. A temperature compensating bearing assembly as claimed in claim 7 in which the expandable helical ceramic member is fabricated from silicon nitride.
US05/434,645 1973-01-19 1974-01-18 Temperature compensating ceramic metal bearing systems Expired - Lifetime US3942847A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
UK2780/73 1973-01-19
GB278073A GB1417244A (en) 1973-01-19 1973-01-19 Temperature compensating ceramic/metal bearing assemblies

Publications (1)

Publication Number Publication Date
US3942847A true US3942847A (en) 1976-03-09

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US (1) US3942847A (en)
DE (1) DE2402382A1 (en)
GB (1) GB1417244A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5947610A (en) * 1997-11-19 1999-09-07 Danieli Wean Hydrodynamic thrust bearing assembly
US6135641A (en) * 1997-10-30 2000-10-24 Honeywell International Inc. Hybrid duplex bearing assembly having thermal compensation
US20090148274A1 (en) * 2007-12-07 2009-06-11 Kostka Richard A Compact bearing support
US20120288368A1 (en) * 2009-12-10 2012-11-15 Hitachi, Ltd. Slide bearing device and compressor
CN103302293A (en) * 2013-05-24 2013-09-18 淮海工学院 Spray deposition densifying device and application thereof

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6191067A (en) * 1984-10-10 1986-05-09 株式会社東芝 Sliding member
DE9001227U1 (en) * 1990-02-03 1990-04-05 H. Krantz Gmbh & Co, 52072 Aachen Combination profile
FR2710114B1 (en) * 1993-09-17 1995-11-17 Renault Hydrodynamic bearing bushing for internal combustion engine.
GB9418973D0 (en) * 1994-09-21 1994-11-09 Rolls Royce Power Eng Bearing assembly

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1204042A (en) * 1958-10-03 1960-01-22 Self-lubricating guide ring
US3150822A (en) * 1961-02-09 1964-09-29 Commissariat Energie Atomique Sealing and centering device for rotary shaft
US3194616A (en) * 1962-01-29 1965-07-13 Saurer Ag Adolph Gas lubricated sleeve bearing for gas turbines
US3238000A (en) * 1962-09-06 1966-03-01 Philips Corp Radial sliding bearing for traversing shafts
US3284144A (en) * 1964-06-08 1966-11-08 American Lava Corp Bearings
US3494674A (en) * 1967-03-31 1970-02-10 Philips Corp Hydrodynamic bearing for axial and radial loads

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1204042A (en) * 1958-10-03 1960-01-22 Self-lubricating guide ring
US3150822A (en) * 1961-02-09 1964-09-29 Commissariat Energie Atomique Sealing and centering device for rotary shaft
US3194616A (en) * 1962-01-29 1965-07-13 Saurer Ag Adolph Gas lubricated sleeve bearing for gas turbines
US3238000A (en) * 1962-09-06 1966-03-01 Philips Corp Radial sliding bearing for traversing shafts
US3284144A (en) * 1964-06-08 1966-11-08 American Lava Corp Bearings
US3494674A (en) * 1967-03-31 1970-02-10 Philips Corp Hydrodynamic bearing for axial and radial loads

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6135641A (en) * 1997-10-30 2000-10-24 Honeywell International Inc. Hybrid duplex bearing assembly having thermal compensation
US5947610A (en) * 1997-11-19 1999-09-07 Danieli Wean Hydrodynamic thrust bearing assembly
US20090148274A1 (en) * 2007-12-07 2009-06-11 Kostka Richard A Compact bearing support
US7857519B2 (en) 2007-12-07 2010-12-28 Pratt & Whitney Canada Corp. Compact bearing support
US20120288368A1 (en) * 2009-12-10 2012-11-15 Hitachi, Ltd. Slide bearing device and compressor
US9255606B2 (en) * 2009-12-10 2016-02-09 Hitachi, Ltd. Slide bearing device and compressor
CN103302293A (en) * 2013-05-24 2013-09-18 淮海工学院 Spray deposition densifying device and application thereof
CN103302293B (en) * 2013-05-24 2014-12-17 淮海工学院 Spray deposition densifying device and application thereof

Also Published As

Publication number Publication date
GB1417244A (en) 1975-12-10
DE2402382A1 (en) 1974-07-25

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